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1.
热层大气密度直接影响低轨道航天器的精密定轨,热层大气密度模型的误差是影响载人航天定轨精度的关键因素。选取400km为载人航天轨道的代表高度,利用CHAMP卫星数据修正热层大气密度模型,进而反演得到2002年的热层大气密度,统计其中长期变化特征,并分析大气密度与太阳活动和地磁活动的关系,得出热层大气密度与两种指数的总体变化趋势一致的结论,且地磁活动与大气密度的相关性更好。同时将大气密度的反演值与神舟三号飞船的实测密度值进行对比,结果显示二者有较好的一致性,其平均残差和均方根误差分别为0.03和0.24,并且地磁平静期的误差明显小于磁暴期。结果表明,利用星载加速度计数据反演载人航天轨道大气密度是一种有效的方法。  相似文献   

2.
This paper gives an overview of the insights into the magnetic reconnection process obtained by in-situ measurements across current sheets found in planetary magnetospheres and the solar wind. Emphasis is placed on results that might be of interest to the study of reconnection in regions where no in-situ observations are available. These results include the role of symmetric versus asymmetric boundary conditions, the identification of the onset conditions, the reconnection rates, and the spatial and temporal scales. Special attention is paid to observations in the so-called diffusion region surrounding the reconnection sites, where ions and eventually also electrons become demagnetized and reconnection is initiated.  相似文献   

3.
Many properties of magnetic reconnection have been determined from in-situ spacecraft observations in the Earth??s magnetosphere. Recent studies have focused on ion scale lengths and have largely confirmed theoretical predictions. In addition, some interesting features of reconnection regions on electron scale lengths have been identified. These recent studies have demonstrated the need for combined plasma and field measurements on electron scale lengths in the reconnection diffusion regions at the magnetopause and in the magnetotail. They have also indicated that measurements, such as those that will be made by the Magnetospheric Multiscale mission in the near future, will have a significant impact on understanding magnetic reconnection as a fundamental plasma process.  相似文献   

4.
原位光固化复合材料纤维铺放制造工艺   总被引:1,自引:0,他引:1  
通过调整紫外光参数和铺放速度参数,制备了相应的NOL环测试件和层合板样件。研究结果表明紫外光原位固化纤维铺放制造工艺是可行的。复合材料具有比强度高、比模量高、抗疲劳性能和耐腐蚀性能优良等优点。随着复合材料的广泛使用,各种高效低成本的制造方法也不断出现。如纤维铺放成型技术、树脂  相似文献   

5.
The Sun is the largest reservoir of matter in the solar system, which formed 4.6 Gyr ago from the protosolar nebula. Data from space missions and theoretical models indicate that the solar wind carries a nearly unfractionated sample of heavy isotopes at energies of about 1 keV/amu from the Sun into interplanetary space. In anticipation of results from the Genesis mission’s solar-wind implanted samples, we revisit solar wind isotopic abundance data from the high-resolution CELIAS/MTOF spectrometer on board SOHO. In particular, we evaluate the isotopic abundance ratios 15N/14N, 17O/16O, and 18O/16O in the solar wind, which are reference values for isotopic fractionation processes during the formation of terrestrial planets as well as for the Galactic chemical evolution. We also give isotopic abundance ratios for He, Ne, Ar, Mg, Si, Ca, and Fe measured in situ in the solar wind.  相似文献   

6.
The heliospheric counterparts of coronal mass ejections (CMEs) at the Sun, interplanetary coronal mass ejections (ICMEs), can be identified in situ based on a number of magnetic field, plasma, compositional and energetic particle signatures as well as combinations thereof. We summarize these signatures and their implications for understanding the nature of these structures and the physical properties of coronal mass ejections. We conclude that our understanding of ICMEs is far from complete and formulate several challenges that, if addressed, would substantially improve our knowledge of the relationship between CMEs at the Sun and in the heliosphere.  相似文献   

7.
This paper develops an analytical, algebraic formalism that predicts effects induced in ring lasers by phase modulation, corresponding both to mode-decoupling mechanisms deliberately incorporated in the ring laser and to naturally occurring periodic or random angular or linear accelerations. The analysis is based on an approach that seems potentially convenient in the analysis of other systems that are physically stable but mathematically nonlinear.  相似文献   

8.
原位自生TiB2/Al复合材料具有密度小、比强度高、高耐磨等特点,在航空航天领域具有广泛的应用前景.主要针对TiB2/Al复合材料车削参数对表面粗糙度的影响进行探索性研究.首先,以车削速度、进给速度、车削深度为对象,基于单因素试验研究了车削参数控制域.进一步在控制域内设计正交试验,并基于试验结果研究了表面粗糙度与车削参数的映射关系,推导了材料去除率模型.最后,以表面粗糙度和材料去除率为优化目标,提出并研究了基于GA-Pareto的车削参数多目标优化方法,并通过试验验证了该方法的可行性和有效性.  相似文献   

9.
分别研究了纯Nb、Nb-25Si和Nb-14Si-26Ti-8Hf-2Cr-2Al的高温氧化行为,并使用X射线衍射仪和透射电镜对氧化膜进行分析。  相似文献   

10.
对热力发动机中存在的线性振荡燃烧的研究,通常假设速度耦合与压力耦合的作用独立无关且作用结果可以线性相加。本文通过对压耦合与速度耦合现象的分析,说明了使这一假设不合理的平均流速界限,并给予了实验证明。  相似文献   

11.
利用Ti-Al-TiO2一CuO体系的放热反应,原位热压合成了Cu掺杂的AJ2O3/TiAl复合材料.借助DSC和XRD研究了Ti-Al-TiO2-CuO体系的反应过程,并采用XRD、SEM研究了复合材料的物相组成及显微结构.结果表明:在Al的开始熔化的同时,Al和CuO的反应开始缓慢进行,并形成CuTix中间产物,放出大量的热,促使Al和TiO2的反应提前,进而使材料在较低温度下致密烧结.CuO掺杂量为6%(质量分数)时所得复合材料弯曲强度可达474 MPa,断裂韧度可达8.89 MPa·m1/2.  相似文献   

12.
GPS/INS组合导航系统松、紧耦合性能比较   总被引:3,自引:0,他引:3  
对GPS/INS组合导航系统的紧耦合算法进行了理论推导。详细分析了当INS元器件性能变差时,GPS/INS组合导航系统在不同耦合模式下的定位精度变化规律,得出采用紧耦合模式的组合导航系统比一般的松耦合方式能获得更好的定位精度;并通过仿真验证了该结论的正确。  相似文献   

13.
机载天线间耦合度分析计算   总被引:2,自引:0,他引:2  
在电磁兼容领域的研究中,时于两副天线所组成的系统的电磁兼容性,用耦合度来描述它们之间的相互作用是非常准确有效的方法.该耦合度由系统中发射天线增益、接收天线增益、天线极化匹配系数、屏蔽系数、发射与接收天线间最短距离等因素决定.仿真计算给出了飞机上不同部位两天线间的耦合系数.  相似文献   

14.
Collisionless microscopic phenomena such as anomalous resistivity, particle acceleration and heat conduction have been successfully treated by particle simulations. Such simulations are usually restricted to volume elements and time scales that are small compared to global scales or even the space and time steps in macroscopic codes. Despite the recent code advances and increases in computing power, it remains necessary to determine the effect of macroscopic dynamics on small scale phenomena and vice versa. The sensitivity of microscopic simulation results to macroscopic boundary conditions is demonstrated. Macroscopic codes, on the other hand, are examined for their dependence on microscopic details. The consequences for the design and analysis of simulation experiments in space physics are discussed. Combining macroscopic and microscopic aspects in a single simulation, despite the usual disparity of scales, will remain a challenging problem.  相似文献   

15.
以软件中数据为核心,通过分析一个具有高度数据耦合、实时并发进程特点的武器装备飞行控制软件实例,提出一种实时软件数据耦合影响分析方法.该方法通过静态分析实时软件中全部共享数据的并发使用情况,可有效发现实时软件中因数据耦合和并发执行引起的共享数据冲突,消除软件的质量隐患.  相似文献   

16.
17.
Theoretical and experimental evidence is collected for additional ionization regions in the mesosphere above lightning discharges and their connection with transient luminous events (TLE). New insights are reported into the different appearances in the Very Low Frequency (VLF) link traces as affected by the mesospheric ionization regions. Based on these findings, physical processes going on in the ionization regions and their coupling to the primary lightning discharge process are conceptualized. Thereafter, some diagnostic potential is outlined. Finally, the ionization regions are considered as a transmitter of secondary low-frequency waves. The distinction is made between the primary electromagnetic waves emitted by the lightning and the secondary waves. As a consequence the Extremely Low Frequency (ELF) and Ultra Low Frequency (ULF) transient signatures observed on the ground are understood as a composite of both wave types. In addition a novel method is introduced to extract the charge moment change of a sprite producing lightning discharge.  相似文献   

18.
风机液力调速控制系统   总被引:2,自引:0,他引:2  
大功率风机采用调整型液力偶合器调整来调节风量具有明显的节能效果。通过对系统的静动特性分析,提出了单处机控制风量流量的闭环控制系统。经过实验,了解了采用PIP调节器的控制系统基本性能及其应用的可能性。  相似文献   

19.
为满足现代航空发动机高空模拟试验燃油流量高精度、快速度的测量要求,针对涡轮流量计不能长期保持校准曲线的缺陷,提出了原位校准技术。重点介绍了原位校准系统的技术要求、主要功能、工作原理、校准装置、工作模式,以及不确定度评估,并进行了对比检验试验。研究结果表明:该系统主要技术指标满足发动机试验需要,测量不确定度满足要求,主要设备具有高的工作可靠性、可控性和稳定性,可实现原位校准和冗余测量功能。  相似文献   

20.
Attention is called to the phenomenon of ?range-Doppler coupling,? characteristic of linear FM (chirp) waveforms, and the strong effect this coupling may have on tracking accuracy. Numerical results are presented for simple three-state filters and for a realistic reentry vehicle tracking problem.  相似文献   

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